Design of the Propeller for Tilt-Rotor UAV

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F18%3A00330438" target="_blank" >RIV/68407700:21220/18:00330438 - isvavai.cz</a>
Result on the web
<a href="https://www.am2018.zcu.cz/" target="_blank" >https://www.am2018.zcu.cz/</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Design of the Propeller for Tilt-Rotor UAV
Original language description
Tilt-wing and tilt-rotor unmanned aerial vehicles (UAVs) represents promising direction for the future development. This paper presents the method for the preliminary design optimization of the propeller for such vehicle. It should be capable to generate high thrust in both forward flight and hover modes. This brings design challenges for the propeller aerodynamic design. All considered variants have same number of blades, engine power, airfoils and diameter. Thrust in forward cruise speed 30 m/s and in hover is computed and compared by the means of Pareto diagram. Choose of the optimal RPM is based on the computation results.
Czech name
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Czech description
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Project
<a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
20th International Conference APPLIED MECHANICS 2018 CONFERENCE PROCEEDINGS
ISBN
978-80-261-0766-8
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
45-48
Publisher name
Západočeská universita
Place of publication
Plzeň
Event location
Myslovice
Event date
Apr 9, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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